# Pratt & Whitney Canada PW207E - Type: Engine model (FAA registry) - Registry code: 52161 - Manufacturer (registry): P&W CANADA - Model: PW207E - Engine type: Turbo-shaft - Power: 646 hp - Data sheet: [TCDS E42NE](https://openairdocs.org/tcds/E42NE) (OpenAirDocs) - Holder: Pratt & Whitney Canada Corp. - Installed in: 9 registered aircraft - Page: https://openairdocs.org/engine/pratt-whitney-canada-pw207e Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2013-03-21](https://openairdocs.org/ad/2013-03-21): Power turbine (PT) disks · Pratt & Whitney Canada PW206B, PW206B2, PW206C and 5 more. Effective Mar 26, 2013 - [AD 2009-03-05](https://openairdocs.org/ad/2009-03-05): Compressor turbine (CT) disc bore · Pratt & Whitney Canada PW206A, PW206B, PW206B2 and 5 more. Effective Mar 27, 2009 - [AD 2004-14-22](https://openairdocs.org/ad/2004-14-22): Automatic low-cycle- fatigue (LCF) · Pratt & Whitney Canada PW206B, PW206C, PW206E and 2 more. Effective Aug 3, 2004 ## Registered aircraft (9) - [N368PA](https://openairdocs.org/aircraft/N368PA): [Papillon Airways Inc](https://openairdocs.org/faa-owner/PAPILLON%20AIRWAYS%20INC), [Boulder City, NV](https://openairdocs.org/faa-place/NV/Boulder%20City), built 1994, S/N 900-00012 - [N714GE](https://openairdocs.org/aircraft/N714GE): [Polar Star Corp](https://openairdocs.org/faa-owner/POLAR%20STAR%20CORP), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), built 1966, S/N 0060 - [N881LT](https://openairdocs.org/aircraft/N881LT): [Ark Angels LLC](https://openairdocs.org/faa-owner/ARK%20ANGELS%20LLC), [Austin, TX](https://openairdocs.org/faa-place/TX/Austin), built 2006, S/N 900-00117 - [N900MH](https://openairdocs.org/aircraft/N900MH): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1993, S/N 900-00008 - [N902GB](https://openairdocs.org/aircraft/N902GB): [Gremlin Air Inc Trustee](https://openairdocs.org/faa-owner/GREMLIN%20AIR%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2001, S/N 900-00089 - [N902LC](https://openairdocs.org/aircraft/N902LC): [Lester E Cox Medical Centers](https://openairdocs.org/faa-owner/LESTER%20E%20COX%20MEDICAL%20CENTERS), [Springfield, MO](https://openairdocs.org/faa-place/MO/Springfield), built 2007, S/N 900-00118 - [N902TX](https://openairdocs.org/aircraft/N902TX): [Burl & Bob Aircraft Leasing LLC](https://openairdocs.org/faa-owner/BURL%20%26%20BOB%20AIRCRAFT%20LEASING%20LLC), [Ashland, OR](https://openairdocs.org/faa-place/OR/Ashland), built 2001, S/N 900-00092 - [N904AF](https://openairdocs.org/aircraft/N904AF): [Leopard Aviation LLC](https://openairdocs.org/faa-owner/LEOPARD%20AVIATION%20LLC), [Ashland, OR](https://openairdocs.org/faa-place/OR/Ashland), built 2001, S/N 900-00101 - [N912LH](https://openairdocs.org/aircraft/N912LH): [Brim Equipment Leasing LLC](https://openairdocs.org/faa-owner/BRIM%20EQUIPMENT%20LEASING%20LLC), [Ashland, OR](https://openairdocs.org/faa-place/OR/Ashland), built 2001, S/N 900-00095 ## NTSB investigations (5) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN15LA066](https://openairdocs.org/ntsb/CEN15LA066), Nov 27, 2014: MD Helicopter MD 900 (N902LC), Highlandville, MO, substantial damage. Probable cause: The pilot's inability to identify the power line during the initial approach in night visual meteorological conditions and his subsequent failure to avoid the power line once he identified it on… - [NTSB CEN09IA032](https://openairdocs.org/ntsb/CEN09IA032), Oct 19, 2008: MD Helicopter MD 900 (N902NM), Amherst, TX, incident, minor damage. Probable cause: The failure of the vertical stabilizer control adapter due to reverse bending fatigue. - [NTSB CEN09IA003](https://openairdocs.org/ntsb/CEN09IA003), Oct 8, 2008: MD Helicopter MD 900 (N902RN), Weatherford, TX, incident, minor damage. Probable cause: The failure of the vertical stabilizer control adapter due to reverse bending fatigue. - [NTSB LAX08IA241](https://openairdocs.org/ntsb/LAX08IA241), Jul 21, 2008: MD Helicopters MD 902 (N902CS), Salinas, CA, incident, minor damage. Probable cause: The pilot's inability to maintain directional control due to the fatigue failure of the threaded portion of the forward directional control cable as a result of the improper installation a lock… - [NTSB ANC06LA038](https://openairdocs.org/ntsb/ANC06LA038), Mar 22, 2006: MD Helicopters MD 900 (N912LH), Mesa, AZ, substantial damage. Probable cause: The manufacturer's inadequate design clearance of the main rotor blade grip pitch cases, which resulted in damage to the pitch cases when they contacted main rotor perimeter bolts during maneuvering… ## FAA accident and incident reports (5) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20141126021509A](https://openairdocs.org/incident/20141126021509A), Nov 26, 2014: Md Helicopter Inc MD 900 (N902LC), Highlandville, MO, Substantial damage. This aircraft was attempting to land in an open field to pick up a passenger that was involved in a vehicle accident and transport the patient to the hospital.… - [Incident 20081003849999I](https://openairdocs.org/incident/20081003849999I), Oct 3, 2008: Doug MD900 (N911AC), Lubbock, TX, Minor damage. (-23) On October 5, 2008, the flight crew of N911AC, was performing flight training under the part 135 certificate at Lubbock international airport. The… - [Incident 20080208842499I](https://openairdocs.org/incident/20080208842499I), Feb 8, 2008: Doug MD900 (N902RN), Gilroy, CA, Minor damage. (-23) In a statement dated 08/03/2008, the pilot [privacy data omitted] states: after departing a rendezous landing area at 75 percent transmission torque in… - [Accident 20060322005049A](https://openairdocs.org/incident/20060322005049A), Mar 22, 2006: Doug MD900 (N912LH), Mesa, AZ, Substantial damage. (-23) During a photo flight northeast of the Mesa ffz, with the pilot and crew chief aboard, the main rotor pitch cases were damaged by contact with the… - [Incident 19971105043419I](https://openairdocs.org/incident/19971105043419I), Nov 5, 1997: Doug MD900 (N900MH), Flagstaff, AZ, Minor damage. Narrative: all time are approximate. Ratings cont. Airplane multiengine, rotorcraft-helicopter, instrument airplane. The flight was a FAA pilot verification of… ## Service difficulty reports (45) As reported by operators and repair stations, by the model named in the report. - [SDR CA160121022](https://openairdocs.org/sdr/CA160121022), Jan 21, 2016: HOSE. CRACKED. (CAN) AFTER SHUT DOWN FOLLOWING A SHORT UNRELATED TEST FLIGHT, TRANSMISSION OIL WAS DISCOVERED COVERING THE TRANSMISSION DECK AND FLOWING DOWN THE SIDES OF THE - [SDR CA151007018](https://openairdocs.org/sdr/CA151007018), Sep 30, 2015: COMPRESSOR. LEAKING. (CAN) THE CREW OF THE HELICOPTER WAS FORCED TO MAKE AN EMERGENCY LANDING ON THE OUTSKIRTS OF PARIS DUE TO LEFT ENGINE LOW OIL PRESSURE AND SMOKE IN THE CABIN. T - [SDR CA150911004](https://openairdocs.org/sdr/CA150911004), Sep 5, 2015: ENGINE. POWER LOSS. (CAN) DURING A FLIGHT TEST, AFTER ANNUAL CHECK, THE NR 1 ENGINE EXPERIENCED A LOSS OF TORQUE. NO OTHER DETAILS ARE AVAILABLE ON THE CIRCUMSTANCES. THE OPERATOR - [SDR CA141008011](https://openairdocs.org/sdr/CA141008011), Sep 21, 2014: THROTTLE. MALFUNCTIONED. (CAN) UPON LANDING, THE PILOT LOWERED THE COLLECTIVE AND 1 ENGINE BEGAN TO ACCELERATE. THE PILOT RAISED THE COLLECTIVE TO APPLY TORQUE TO REDUCE ENGINE SPEED. T - [SDR QMLA2014012214010](https://openairdocs.org/sdr/QMLA2014012214010), Jan 22, 2014: TRANSMISSION. MAKING METAL. MULTIPLE MAIN TRANSMISSION CHIP LIGHTS, AFTER FOLLOWING CSP 900RMM 2 CHAPTER 63-20-00 & TABLE 601. CHIPS INDICATED ALL UNDER THE LIMITS OF THE CHAPTER BUT COME - [SDR CA130729002](https://openairdocs.org/sdr/CA130729002), Jul 15, 2013: ENGINE. POWER LOSS. (CAN) AFTER DROPPING A SLINGED LOAD, THE NR 2 ENGINE FROZE AT HIGH TORQUE FOR 20 SEC. THE NR 1 ENGINE REDUCED POWER ACCORDINGLY BUT THE MAIN ROTOR OVERSPED TO 1 - [SDR CA130617002](https://openairdocs.org/sdr/CA130617002), Jun 10, 2013: ENGINE. SHUTDOWN. (CAN) THE PILOT REPORTED AN ELECTRONIC ENGINE CONTROL SHUTDOWN FROM THE LT ENGINE. THE PILOT REQUESTED MORE POWER FROM RT ENGINE TO FLY OVER THE CABLES IN FRONT - [SDR CA130508014](https://openairdocs.org/sdr/CA130508014), May 3, 2013: SCREW. MISSING. (CAN) FOD DAMAGE TO NOTAR FAN. STATOR BLADE RETAINER SCREW FOUND MISSING. - [SDR CA121211003](https://openairdocs.org/sdr/CA121211003), Dec 3, 2012: COMPRESSOR. SEIZED. (CAN) CREW COMPLAINED OF POPPING NOISE WHEN GOING FROM IDLE TO FLY CONDITION. MECHANIC CONFIRMED NOISE AND COMMENCED COMPRESSOR WASHES AND RINSES. DURING THE RI - [SDR CA120716009](https://openairdocs.org/sdr/CA120716009), Jul 8, 2012: BLADE. FRACTURED. (CAN) AFTER TAKINGOFF FROM THE ROOF OF A HOSPITAL, DURING THE TRANSITION PHASE, THE CREW HEARD A LOUD NOISE FOLLOWED BY A POWER LOSS AND NR 1 ENGINE SHUTDOWN. T - [SDR QMLA2011050911056](https://openairdocs.org/sdr/QMLA2011050911056), May 9, 2011: IMPELLER. DAMAGED. PART OF THE GASKET OF THE INLET SCREEN CAME LOOSE AND WAS INGESTED INTO THE ENGINE. ONE BLADE ON THE COMPRESSOR HAD DAMAGE THAT CAUSED A LOUD WHINING NOISE WHEN - [SDR 2009FA0000440](https://openairdocs.org/sdr/2009FA0000440), Jan 30, 2009: DRIVE SHAFT. CORRODED. DURING AN ANNUAL INSP THE MAIN ROTOR DRIVE SHAFT AND DRIVE PLATE WHERE REMOVED TO SATISFY THE 12 MONTH REQUIREMENT. WHILE REMOVING THE DRIVE SHAFT IT WAS FOUND - [SDR 2006FA0000620](https://openairdocs.org/sdr/2006FA0000620), Jun 8, 2006: HOSE. CRACKED. PILOT NOTICED TRANSMISSION OIL PRESSURE INDICATION DROPPED FROM GREEN TO YELLOW TO RED. MADE UNSCHEDULED LANDING. FOUND FWD LT TRANSMISSION OIL COOLER HOSE LEAK - [SDR 2006FA0000503](https://openairdocs.org/sdr/2006FA0000503), May 16, 2006: HOSE. CRACKED. DISCOVERED MAIN TRANSMISSION OIL HOSE FROM OIL COOLER TO MAIN TRANSMISSION LEAKING FROM STEEL BRAIDING. PULLED BACK BRAIDING AND FOUND HOSE TO BE CRACKED. REPLA - [SDR 2006FA0000506](https://openairdocs.org/sdr/2006FA0000506), May 16, 2006: HOSE. CRACKED. DISCOVERED MAIN TRANSMISSION OIL HOSE FROM OIL COOLER TO MAIN TRANSMISSION LEAKING FROM STEEL BRAIDING. PULLED BACK BRAIDING AND FOUND HOSE TO BE CRACKED. REPLA - [SDR 2006FA0000507](https://openairdocs.org/sdr/2006FA0000507), May 16, 2006: BEAM. CRACKED. DURING SCHEDULED INSPECTION FOUND FLEXBEAM CRACKED IN LEG OF FLEXBEAM. REJECTED FLEXBEAM IAW INSPECTION CRITERIA IN MAINTENANCE MANUAL. REPLACED WITH NEW FLEXBE - [SDR 2006FA0000508](https://openairdocs.org/sdr/2006FA0000508), May 16, 2006: BEAM. CRACKED. DURING SCHEDULED INSPECTION FOUND FLEXBEAM CRACKED IN LEG OF FLEXBEAM. REJECTED FLEXBEAM IAW INSPECTION CRITERIA IN MM. REPLACED WITH NEW FLEXBEAM. - [SDR 2006FA0000501](https://openairdocs.org/sdr/2006FA0000501), May 16, 2006: OIL COOLER. LEAKING. FOUND WETTING OIL MAIN TRANSMISSION/ENGINE OIL COOLER CORE. REMOVED AND SENT OUT FOR EVALUATION. COOLER FOUND TO HAVE INTERNAL CORROSION THAT CAUSED MATERIAL LO - [SDR L192006F00000](https://openairdocs.org/sdr/L192006F00000), Apr 14, 2006: LINE. WORN. ON TRAINING FLIGHT, RT ENG FIRELIGHT CAME ON. PILOT COMPLIED WITH EMERGENCY PROCEDURES, THEN SHUT RT ENG DOWN AND DISCHARGED RT ENG FIRE BOTTLE, LANDED AC AND F - [SDR 2006FA0000274](https://openairdocs.org/sdr/2006FA0000274), Mar 1, 2006: HOSE. CRACKED. HOSE IS INSTALLED ON MD902 HELICOPTERS. MD P/N IS 900D3409526-105. HOSE IS USED FOR MAIN TRANSMISSION OIL COOLING. FOUND LARGE ACCUMULATION OF OIL ON TRANSMISSI - [SDR 2005FA0000816](https://openairdocs.org/sdr/2005FA0000816), Jun 8, 2005: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD 2002-10-05- MAIN ROTOR UPPER HUB INSP FOUND (2) BOLT HOLES CRACKED AS DEPICTED IN MD HELICOPTERS SERVICE BULLETIN 900-072. CRACKS WE - [SDR 2004FA0000938](https://openairdocs.org/sdr/2004FA0000938), Dec 16, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD 2002-10-05 "MAIN ROTOR UPPER HUB INSP" FOUND BOLT HOLES CRACKED AS DEPICTED IN MD HELICOPTERS SERVICE BULLETIN 900-072. PART TOTAL T - [SDR 2004FA0000940](https://openairdocs.org/sdr/2004FA0000940), Dec 16, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF A.D. 2002-10-05 " MAIN ROTOR UPPER HUB INSP." FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN MD HELICOPTERS SERVICE BULLETIN 9 - [SDR 2004FA0000939](https://openairdocs.org/sdr/2004FA0000939), Dec 16, 2004: BEAM. CRACKED. DURING 100 HOUR INSPECTION, FOUND FLEX BEAM CRACKED IN AREA OF LEG GOING INTO UPPER HUB. REPLACED PART WITH UPDATED SERVICEABLE PART. - [SDR 2004FA0000934](https://openairdocs.org/sdr/2004FA0000934), Dec 16, 2004: FUEL CELL. LEAKING. DURING TROUBLESHOOTING A FUEL LEAK FOUND THAT WHEN THE FUEL CELL WAS FLEXED, FUEL WOULD WEEP FROM EXTERIOR SURFACE. REMOVED FUEL CELL AND SENT OUT FOR TEST AND - [SDR PG9R097903](https://openairdocs.org/sdr/PG9R097903), Oct 21, 2004: LINE. LEAKING. FOUND TO BE LEAKING A SMALL QUANTITY OF OIL/REPLACED OIL HOSE ASSY. - [SDR PG9R97903](https://openairdocs.org/sdr/PG9R97903), Oct 21, 2004: LINE. LEAKING. FOUND TO BE LEAKING A SMALL QUANTITY OF OIL/ REPLACED OIL HOSE ASSY. (K) - [SDR 2004FA0000877](https://openairdocs.org/sdr/2004FA0000877), Oct 12, 2004: ROTOR HEAD. CRACKED. HAD VIBRATION (.7 IPS) CAUTION ON IDS DURING FLIGHT AND HIGH VIBRATION ON SHUT DOWN BETWEEN 30-40 PERCENT NR. INSPECTED MAIN ROTOR SYSTEM IAW MAINTENANCE MANUAL - [SDR 2004FA0000802](https://openairdocs.org/sdr/2004FA0000802), Oct 12, 2004: DRIVE SHAFT. WORN. DURING ACCOMPLISHMENT OF A 300 HR INSPECTION FOUND MAIN ROTOR DRIVE SHAFT UPPER DRIVE SPLINES WORN BEYOND MAINTENANCE MANUAL LIMITS. PART TOTAL TIME: 1478.9 HRS - [SDR 2004FA0000578](https://openairdocs.org/sdr/2004FA0000578), Jul 19, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF A.D. 2002-10-05, (MAIN ROTOR UPPER HUB INSP.) FOUND (2) OUT OF (10) HOLES CRACKED IN UPPER HUB FLANGE AS DEPICTED IN MFG SERVICE BULLET - [SDR 2004FA0000876](https://openairdocs.org/sdr/2004FA0000876), Jul 19, 2004: ROTOR HEAD. CRACKED. DURING ACCOMPLISHMENT OF AD 2002-10-05, "MAIN ROTOR UPPER HUB INSP", FOUND (2) OUT OF (10) HOLES CRACKED IN UPPER HUB FLANGE AS DEPICTED IN MD HELICOPTERS SERVI - [SDR 2004FA0000324](https://openairdocs.org/sdr/2004FA0000324), Apr 21, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD 2002-10-05 (MAIN ROTOR UPPER HUB INSPECTION), FOUND (3) OUT OF (10) BOLT HOLES TO BE CRACKED AS DEPICTED IN MFG SERVICE BULLETIN 900 - [SDR 2004FA0000322](https://openairdocs.org/sdr/2004FA0000322), Apr 13, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD2002-10-05 (MAIN ROTOR UPPER HUB INSP.) FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN MFG SERVICE BULLETIN 900-072. CRACKS - [SDR 2004FA0000323](https://openairdocs.org/sdr/2004FA0000323), Apr 13, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD2002-10-05 (MAINROTOR UPPER HUB INSP.) FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN MFG SERVICE BULLETIN 900-072. CRACKS S - [SDR 2004FA0000332](https://openairdocs.org/sdr/2004FA0000332), Apr 13, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD2002-10-05 (MAINROTOR UPPER HUB INSP.) FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN MFG SERVICE BULLETIN 900-072. CRACKS S - [SDR 2004FA0000331](https://openairdocs.org/sdr/2004FA0000331), Apr 13, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD 2002-10-05 (MAIN ROTOR UPPER HUB INSP.) FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN SERVICE BULLETIN 900-072. CRACKS STA - [SDR 2004FA0000801](https://openairdocs.org/sdr/2004FA0000801), Apr 13, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD 2002-10-05, MAIN ROTOR UPPER HUB INSP. FOUND (3) OUT OF (10) BOLT HOLES CRACKED AS DEPICTED IN SB 900-072. CRACKS START IN BOLT HOLE - [SDR 2004FA0000330](https://openairdocs.org/sdr/2004FA0000330), Mar 3, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF AD 2002-10-05 INSP. (MAIN ROTOR UPPER HUB INSP.) FOUND (2) OUT OF (10) FLANGE BOLT HOLES WITH CRACKS AS DEPICTED IN MFG SERVICE BULLETI - [SDR 2004FA0000163](https://openairdocs.org/sdr/2004FA0000163), Feb 4, 2004: LINE. CRACKED. AIRCRAFT EXPERIENCED LOW TRANSMISSION OIL PRESSURE. DURING RUN-UP AND LEAK CHECK FOUND TRANSMISSION OIL COOLER LINE P/N 900D3409526105 TO BE LEAKING FROM UNDER - [SDR 2004FA0000095](https://openairdocs.org/sdr/2004FA0000095), Jan 8, 2004: HUB. CRACKED. DURING ACCOMPLISHMENT OF A.D. 2002-10-05(MAIN ROTOR UPPER HUB INSPECTION)FOUND (6) OUT OF (10) UPPER FLANGE BOLT HOLES TO BE CRACKED. CRACKS RUN RADIALLY FROM B - [SDR 2003FA0000190](https://openairdocs.org/sdr/2003FA0000190), Sep 17, 2001: FILTER. CONTAMINATED. BYPASS PIN POPPED ON NR 1 HYDRAULIC RETURN FILTER. REMOVED FILTER AND INSPECTED FOR CONTAMINATION. REPLACED FILTER. OPS AND LEAK CHECK GOOD. - [SDR 2003FA0000188](https://openairdocs.org/sdr/2003FA0000188), Sep 6, 2001: INDICATOR. DEFECTIVE. AFTER INSTALLING NEW HYDRAULIC FILTER, THE RETURN SIDE BYPASS INDICATOR POPPED WITH NO PRESSURE APPLIED. AFTER RESETTING THE INDICATOR, INDICATOR POPPED AGAIN. - [SDR 2003FA0000187](https://openairdocs.org/sdr/2003FA0000187), Jul 26, 2001: DRIVE LINK. WORN. MAIN ROTOR UPPER DRIVE LINK BEARING PLAY EXCEEDS MAINTENANCE MANUAL LIMITS. - [SDR 2003FA0000186](https://openairdocs.org/sdr/2003FA0000186), Jul 24, 2001: DRIVE LINK. WORN. MAIN ROTOR UPPER DRIVE LINK BEARING PLAY EXCEEDS MAINTENANCE MANUAL LIMITS. - [SDR 2003FA0000184](https://openairdocs.org/sdr/2003FA0000184), Jun 23, 2001: TRANSMISSION. MAKING METAL. MAIN TRANSMISSION PRODUCING METAL CHIPS. CHIP SIZE EXCEED MAINTENANCE MANUAL LIMITS. ## PMA parts (OpenAirDocs) (107, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first. - [3014422AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157889633320250310190842.0001): Packing with Retainer. Aero Attitude, LLC · PMA PQ00001CB · Replaces PWC 3014422 · Feb 25, 2025 - [3015234AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130436253520240919140838.0001): Nut, Self-Locking, Shank. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3015234, 3015233, 3015232, 3016299… · Aug 7, 2024 - [RM3022375](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105341282120230503123952.0001): Seal, Plain. Rimark Manufacturing · PMA PQ10018NE · Replaces 3022375 · Apr 19, 2023 - [CH92106-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID894244232820210610203815.0001): Exciter-Ignition. Champion Aerospace LLC · PMA PQ1287CE · Replaces 3043937-09 · Feb 2, 2021 - [8063-115](https://drs.faa.gov/browse/excelExternalWindow/58E47C9831427D2B8625844800514B86.0001): Fuel Metering Unit. Woodward Inc · PMA PQ2020CE · Replaces 3053928-04 · Jun 17, 2018 - [CH92106-2](https://drs.faa.gov/browse/excelExternalWindow/849AECF9E09B91B9862582960070BA94.0001): Exciter Assembly. Champion Aerospace LLC · PMA PQ1287CE · Replaces 3043937-07 3043937-05 3043937-03… · Mar 21, 2018 - [GM9271](https://drs.faa.gov/browse/excelExternalWindow/DF005AAC3289C92986257FAA0067F4D2.0001): Linear Transducer. Kavlico Corporation · PMA PQ1186NM · Replaces 03X-3039635 · Jan 12, 2016 - [GM9271](https://drs.faa.gov/browse/excelExternalWindow/590F3B03A30BFAE386257EF40064536F.0001): Linear Transducer. Kavlico Corporation · PMA PQ1186NM · Replaces 03X-3039635 · Sep 21, 2015 - [572744-28](https://drs.faa.gov/browse/excelExternalWindow/7EB29D49BA73463986257C23007821F2.0001): Fuel Filter Element Assembly. Purolator Facet Inc (formerly Facet Filter Products) · PMA PQ1207CE · Replaces Pratt & Whitney Canada P/N 3070220-01… · May 29, 2013 - [1742974-01](https://drs.faa.gov/browse/excelExternalWindow/6AA0CE287217996086257C23007821EF.0001): Oil Filter Element Assembly. Purolator Facet Inc (formerly Facet Filter Products) · PMA PQ1207CE · Replaces Pratt & Whitney Canada P/N 3107548-01… · May 29, 2013 - [ACB093F2480Y1](https://drs.faa.gov/browse/excelExternalWindow/DDDC057B6D9330B486257A010056FF97.0001): Filter Element. Pall Aeropower Corporation · PMA PQ1063CE · Replaces 5903150 · Feb 26, 2012 - [AC9806F30Y1](https://drs.faa.gov/browse/excelExternalWindow/DB34BECA3A4C7E4886257A010056FEF3.0001): Lube Oil Filter Element. Pall Aeropower Corporation · PMA PQ1063CE · Replaces 1A5074 · Feb 26, 2012 - [88043-1](https://drs.faa.gov/browse/excelExternalWindow/498C3450925C899A8625788B007321CB.0001): Rotor AC. Pacific Scientific, OECO · PMA PQ0076NM · Replaces 3038627 · Apr 19, 2011 - [88042-1](https://drs.faa.gov/browse/excelExternalWindow/154C2333AAAA6EE88625788B007321F7.0001): Stator AC Generator. Pacific Scientific, OECO · PMA PQ0076NM · Replaces 3038628 · Apr 19, 2011 - [6970-042](https://drs.faa.gov/browse/excelExternalWindow/88AB65A94DEBCB94862577A800620420.0001): Pump-fuel. Woodward Inc · PMA PQ2020CE · Replaces Pratt and Whitney Canada Corp P/N… · Sep 13, 2010 - [6970-001](https://drs.faa.gov/browse/excelExternalWindow/32A97566C7DA369D862577A8006203F1.0001): Pump-fuel. Woodward Inc · PMA PQ2020CE · Replaces Pratt and Whitney Canada Corp P/N… · Sep 13, 2010 - [CH92106](https://drs.faa.gov/browse/excelExternalWindow/E0535DFDD4F2B1D9862576B2004E2397.0001): Exciter Assembly. Champion Aerospace LLC · PMA PQ1287CE · Replaces 3043937-05 · Dec 8, 2009 - [CH92106](https://drs.faa.gov/browse/excelExternalWindow/FC944A35EAB8532C8625766D006FAFC9.0001): Exciter Assembly. Champion Aerospace LLC · PMA PQ1287CE · Replaces 3043937-05 · Oct 5, 2009 - [8063-174](https://drs.faa.gov/browse/excelExternalWindow/BE3C40959BBD850B862573FB0057D0A1.0001): Flow Divider Assy. Woodward Inc · PMA PQ2020CE · Replaces Pratt and Whitney Canada 3044134-03 · Jan 14, 2008 - [6970-042](https://drs.faa.gov/browse/excelExternalWindow/7CFA2F500A6FF48D862573FB0057D0E3.0001): Fuel- Pump. Woodward Inc · PMA PQ2020CE · Replaces Pratt and Whitney Canada 3058147-02 · Jan 14, 2008 - [JE00073-2](https://drs.faa.gov/browse/excelExternalWindow/ED8F4DC04E8DBFC586257284005E4551.0001): Bearing. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1B5428CL2 · Oct 11, 2006 - [JE00073-1](https://drs.faa.gov/browse/excelExternalWindow/C5084370B81601B086257284005E4515.0001): Bearing. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1B5428CL1 · Oct 11, 2006 - [JW00023](https://drs.faa.gov/browse/excelExternalWindow/BBFABB6386D38E9086257284005E54D9.0001): Washer. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1B5429 · Oct 11, 2006 - [JK00133](https://drs.faa.gov/browse/excelExternalWindow/7D0EBE5540055AFD86257284005E55D2.0001): Key Spacer. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 8A1530 · Oct 11, 2006 - [JK00133-02](https://drs.faa.gov/browse/excelExternalWindow/567E21278E43354386257284005E564B.0001): Key Spacer. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 8A2839-02 · Oct 11, 2006 - [JK00108](https://drs.faa.gov/browse/excelExternalWindow/2BE6BE99C7B89BA586257284005E2F64.0001): Pin, Shoulder Headless. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1B7168 · Oct 11, 2006 - [JK00133-01](https://drs.faa.gov/browse/excelExternalWindow/08D86C2269CEB77D86257284005E560D.0001): Key Spacer. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 8A2839-01 · Oct 11, 2006 - [JE00073](https://drs.faa.gov/browse/excelExternalWindow/001B568A9463DC4986257284005E44D6.0001): Bearing. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1B5427 · Oct 11, 2006 - [113758](https://drs.faa.gov/browse/excelExternalWindow/F6D3BA88BB5966668625718C006F95F1.0001): Hose-NM, 4375-20 X 7.690. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5691 · Jun 8, 2006 - [109569-1](https://drs.faa.gov/browse/excelExternalWindow/EDB4F89E2AB580E28625718C006F9272.0001): Hose-Hydraulic, Compr. Stator. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1A9357 · Jun 8, 2006 - [113674-4](https://drs.faa.gov/browse/excelExternalWindow/E99C4D7FE39649118625718C006F953C.0001): Hose-NM, .750 Tube X 7.050. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5364 · Jun 8, 2006 - [109569-3](https://drs.faa.gov/browse/excelExternalWindow/DD187A7C3A95E3B18625718C006F9313.0001): Hose-NM, Return, Compr. Stator Cyl.. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1A9359 · Jun 8, 2006 - [109666](https://drs.faa.gov/browse/excelExternalWindow/D414B3E6095172C58625718C006F9345.0001): Hose & Tube-CLG Oil, IDGS Cooler. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B0148 · Jun 8, 2006 - [97883-5](https://drs.faa.gov/browse/excelExternalWindow/D08F3B5E65398D908625718C006F942C.0001): Hose - 1.000 X 2.500. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1A5941 · Jun 8, 2006 - [113677-2](https://drs.faa.gov/browse/excelExternalWindow/AD5A3EE05B09E25B8625718C006F95CA.0001): Hose & Tube-NM Return, Air SOV. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5387 · Jun 8, 2006 - [113674-3](https://drs.faa.gov/browse/excelExternalWindow/ACA8D338E11321CA8625718C006F9513.0001): Hose-NM, .750 Tube X 7.500. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5367 · Jun 8, 2006 - [113676-2](https://drs.faa.gov/browse/excelExternalWindow/AA24138EF57BF26F8625718C006F9596.0001): Hose & Tube-NM Return, Air SOV. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5378 · Jun 8, 2006 - [110678](https://drs.faa.gov/browse/excelExternalWindow/A86430C9ADF46E8F8625718C006F93FA.0001): Hose-NM, .437-20-20 X 11.530. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B3415 · Jun 8, 2006 - [113674-2](https://drs.faa.gov/browse/excelExternalWindow/7C84CC1BE1F5B24B8625718C006F964C.0001): Hose-NM, .750 Tube X 12.750. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5399 · Jun 8, 2006 - [113676-1](https://drs.faa.gov/browse/excelExternalWindow/7BEB1FC4EAB5CD838625718C006F9568.0001): Hose & Tube-NM, Hydr., Air SOV. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5381 · Jun 8, 2006 - [109873](https://drs.faa.gov/browse/excelExternalWindow/79110FDDA92959B08625718C006F93A2.0001): Hose-PB, EEC. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B2159 · Jun 8, 2006 - [109993](https://drs.faa.gov/browse/excelExternalWindow/7228F761C1A93A658625718C006F93D1.0001): Hose & Tube-PT2, EEC. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B1508 · Jun 8, 2006 - [109707](https://drs.faa.gov/browse/excelExternalWindow/6EAC3E24388BA5EB8625718C006F9370.0001): Hose & Tube-CLG Oil, IDGS Air Cooler. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B0030 · Jun 8, 2006 - [97883-9](https://drs.faa.gov/browse/excelExternalWindow/5BE35901803A337D8625718C006F948B.0001): Hose 1.500 X 2.250. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B1249 · Jun 8, 2006 - [113762](https://drs.faa.gov/browse/excelExternalWindow/55647ED6646FBEF78625718C006F961A.0001): Hose & Tube-NM. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5768 · Jun 8, 2006 - [113673-1](https://drs.faa.gov/browse/excelExternalWindow/42FD612B92D036858625718C006F94EB.0001): Hose-NM, .750 Tube X 13.300. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B5390 · Jun 8, 2006 - [109569-2](https://drs.faa.gov/browse/excelExternalWindow/319629BFE4DDD1348625718C006F92EA.0001): Hose & Tube -Hydraulic Compr. Stator. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1A9358 · Jun 8, 2006 - [97883-8](https://drs.faa.gov/browse/excelExternalWindow/2903BB3490D2ACD78625718C006F9455.0001): Hose 1.000 X 2.000. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 1B1248 · Jun 8, 2006 - [X218-104](https://drs.faa.gov/browse/excelExternalWindow/1D73BB565D8EF0D08625718C006F94BC.0001): Clamp-loop, 1.546, Cushion. Smith Tubular Systems - Laconia Inc · PMA PQ0287NE · Replaces 450952 · Jun 8, 2006 - [794434SD](https://drs.faa.gov/browse/excelExternalWindow/21A49AF54AEAB916862571D3004FDE16.0001): Packing, Preformed. Seal Dynamics Inc · PMA PQ1715CE · Replaces Pratt & Whitney 794434 · Mar 21, 2006 All of them: https://openairdocs.org/engine/pratt-whitney-canada-pw207e/pma.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.